Apparatus for and method for accelerating fluidized particulate matter

ABSTRACT

A fluid jet accelerator/pressurizer apparatus for accelerating and pressurizing a fluidized stream of particulate matter, e.g. for ice blasting, has a nozzle housing defining a main conduit, forming a passage for the flow of the fluidized stream through the nozzle housing. The main conduit has a constriction formed by a convergent-divergent region of the main conduit for effecting acceleration of the fluidized stream, and an inner blast nozzle is provided in the main conduit and directed in a downstream direction towards the constriction. In operation, a blast medium is discharged from the inner blast nozzle at a speed sufficient to form within the fluidized stream a flow front which is impenetrable by the fluidized stream and which co-operates with the constriction to accelerate the fluidized stream.

This application is the U.S. national stage application of PCTapplication PCT/CA95/00115 filed Feb. 28, 1995. This application is alsoa continuation-in-part of U.S. application Ser. No. 08/203,584 filedMar. 1, 1994.

TECHNICAL FIELD

This invention relates to an apparatus for and a method of acceleratingand pressurizing a fluidized stream of particulate matter for thepurposes, for example, of duct transport over long distances and for thedischarge of the fluidized streams at high velocities.

BACKGROUND ART

In abrasive blast cleaning, such as with sand, grit or shot particles,velocity is imparted to particles which are directed against a surfaceto be cleaned, depainted, radioactively decontaminated or otherwisemodified. The dynamic particle energy is converted into destructiveforces which mechanically abrade or deform surface coatings. Thismethodology results in residual particulate matter of the blast stream,blast medium and the material removed as the blasting strips off thecoating of the target surface, creating a high dust environment that maybe hazardous to health, equipment and surrounding property. The cost ofremoving such matter may be excessive as well.

In addition, these blast particles are destructive when used for thetreatment of fragile surfaces such as thin sheets, carbon and plastic.

Recently, less aggressive particulate matter such as dry ice and waterice has been utilized as blast particulate matter to avoid theseproblems, but not without limitations relating to transport anddischarge. First, ice is not free flowing and must be "fluidized" with agas, liquefied gas or liquid in order to be transported to the targetsurface. Second, ice is not effective if discharged at low velocities.Third, ice is friable and heat sensitive and high velocity transportwill generate considerable friction and heat and cause melting andbreakdown of the ice particles. That said, the aim has been to achievelow transport and high discharge velocities within an apparatus that canhandle all practical and useful types and sizes of particulate matter,including ice particles, and to control the sizing of particulatematter.

Previous practice of transporting or discharging fluidized particulatematter at high pressures, high velocities or both has involved the useof costly mechanical positive displacement pumps, which are volumedependent, complicated and do not mix or disperse or accelerate afluidized stream well. Blowers, fans, and air jet and liquid jet pumpshave also been used, but are only capable of generating small pressureincreases and low velocities.

The use of single venturi nozzles as described in U.S. Pat. Nos.4,038,786 and 4,707,951, in "Foundations of Aerodynamics" (A. M. Kuetheand J. D. Schetzer) and the "Mechanical Engineers' Handbook" (T.Baumeister and L. S. Marks) is ineffective for increasing pressure ascan be achieved by induced flow created by injectors using either gas orliquid. Single venturi nozzles create increased velocity by gasexpansion through falling pressures.

Amplifiers, such as taught by U.S. Pat. No. 4,389,820, have been usedwith limited success to induce flow in significant volumes, butunfortunately are able to generate only minimal pressure differentialsand small increases in velocity. This is due to several inherentproblems. First, the induction effect is dependent upon the boundarylayer formation of a very thin high speed air film which is destroyed bythe bombardment of particulate matter. Second, since the induction isvia boundary layer shear viscous forces, there is minimal mixing andtherefore little energy transfer to the bulk of the induced stream.Third, acceleration by usage of conduit restrictions will greatly affector destroy the inductive effect, thereby placing a limitation on theeffective increase in velocity that may be achieved. Fourth, airamplifiers, as the name implies, use a small amount of high velocity airto form a boundary layer to induce flow of a much larger amount of airand therefore there is little energy available to be transferred eitherfor pressure or velocity increase. Finally, the foregoing limitations inmixing, velocity, available energy and pressure all preclude thepossibility for effective high velocity discharge.

Oblique injectors of the form utilized in U.S. Pat. Nos. 4,555,872 and5,203,794, where air or liquid is introduced via an opening in a mainconduit after or before the entry of a particulate stream into the mainconduit, have the chief advantage of providing for maximal turbulenceand good mixing. However, these effects disturb the natural flow patternof any incoming particulate stream, thereby preventing the possibilityof forming an efficient nozzle. Because of this loss of efficiency, moreenergy and significant expense are required to achieve optimal pressuresand velocities. The disturbance of the natural flow also results inregions of different velocities, thereby causing particulate depositionand plugging, erosion in the apparatus, and unwanted damage to friable,delicate particles including excessive size reduction.

As a variation of these injectors, gas or liquid injectors embodiedwithin nozzles that extend into the main conduit thereby creating amulti-nozzle system have been practised in the art (U.S. Pat. Nos.998,762, 4,806,171, and 4,817,342). In terms of discharge effectiveness,these systems use inefficient non-venturi converging nozzles, whichrelease an uncontrolled expanded blast pattern. This pattern tends toconcentrate the bulk of the particulate matter in a central region andconsequently are not suitable for targeting large blast areas. The samemay be said of component attachments such as are described in U.S. Pat.No. 4,843,770, which attempt to create a wider blast area using anuncontrolled expanded blast pattern. In addition, these systems tend toplug easily due to the use of non-fluid path defining nozzle bodyprofiles, which create regions of different velocities and depositions.

In the U.S. Pat. No. 998,762, there is disclosed an apparatus forcombining comminuted solids and liquids in which an internally rifledair nozzle discharges an air jet into a stream of solid particles, whichthen passes through a further nozzle. Both of the nozzles comprise apassage converging to an outlet mouth, so that the flow beyond theoutlet mouths of the nozzles is uncontrolled. Consequently, the flowbeyond the nozzle mouths is allowed to expand freely, to undergoturbulence and to produce excessive mixing, all of which will consumeenergy that could otherwise be directed for other purposes, and inparticular for the acceleration of the solids.

DISCLOSURE OF THE INVENTION

According to the present invention, there is provided a method ofaccelerating and pressurizing a fluidized stream of particulatematerial, comprising causing the stream flow through a constriction in amain conduit and discharging a flow of blast medium towards theconstriction, characterized in that the blast medium is accelerated to asupersonic speed before being discharged into the fluidized stream andforms within the fluidized stream a flow front which is impenetrable bythe fluidized stream and which co-operates with the constriction toaccelerate the fluidized stream.

The acceleration of the blast medium may be effected by means of aconstriction in a flow passage for the blast medium.

By supplying the blast medium at sonic speed to the constriction in theblast medium passage, the blast medium can be accelerated to supersonicspeed, and shock fronts are then formed in the blast medium, downstreamof the blast medium passage, within the flow front. In this way there isformed within the fluidized stream an impenetrable volume which isdefined by the flow front and which tapers downstream into the mainconduit constriction so as to define therewith a virtual or effectiveLaval nozzle through which the fluidized stream is accelerated.

After passing through the throat of the virtual Laval nozzle, thefluidized stream is allowed to expand in a controlled manner, and maythen be passed through a further constriction and thereby furtheraccelerated and shaped for discharge as a spray, or may alternatively befed further along the main conduit for subsequent further acceleration.

The present invention also provides a fluid accelerator and pressurizerapparatus for accelerating and pressurizing a fluidized stream ofparticulate matter, comprising a nozzle housing defining a main conduitfor the flow of the fluidized stream, and a blast nozzle located in themain conduit and having an outlet end portion directed towards aconstriction in the main conduit for discharging a blast medium throughthe constriction, characterized by a constriction in a passage for theflow of said blast medium through the blast nozzle for accelerating theblast medium to supersonic speed and thereby forming in the main conduita flow front which is impenetrable by the fluidized stream and whichco-operates with the constriction in the main conduit to form aneffective nozzle for accelerating the fluidized stream.

The present fluid accelerator and pressurizer apparatus operates on thebasis of a reduced pressure at an inlet of a main conduit in order topromote the feeding of the fluidized stream into the apparatus and anincreased pressure on an outlet side in order to compensate forsubsequent transport duct resistance or to provide for increasedacceleration and velocity through expansion. The structures andassociated functions within the present apparatus are designed to createdifferential pressures and differential velocities which entrain,disperse and establish conditions for promoting energy transfer betweenthe incoming fluidized stream and the blast medium, which may comprisegas, such as air, or liquified gas, such as liquified air.

Preferably, the main conduit has a wall spaced from the blast nozzle,and the blast nozzle includes a fairing extending around the blastnozzle, the fairing having a streamlined shaped for promotingstreamlined flow of the fluid liquid past the blast nozzle.

In a preferred embodiment of the invention, the fairing is profiled toprovide an aerodynamic and hydrodynamic shape, the main conduit beinginternally profiled to provide a first venturi nozzle prior to contactbetween the fluidized stream and the blast nozzle. The inner blastnozzle may be secured by means of the fairing to the wall of the mainconduit, which fairing together with the external profile of the innerblast nozzle provide a guided free-flowing flow path free of velocitydifferentials and plugging. A divergence and acceleration region mayalso be created by the discontinuance of the fairing within the mainconduit space. Finally, at some distance downstream from the inner blastnozzle, the internal profile of the main conduit is shaped to form theconstruction as a second venturi nozzle and acceleration region.

For discharge, the apparatus may have a discharge nozzle whichfacilitates a controlled expansion of the fluidized stream, therebycreating a more even blast pattern and promoting better kinetic energytransfer between the blast medium and particulate matter and thus,promoting greater particulate discharge velocities. Without thedischarge nozzle, the apparatus can be used to convey and boost thefluidized stream to overcome subsequent transport duct resistance overlong distances until the fluidized stream is finally discharged againsta target surface.

In terms of construction, all high pressure conduits may be built fromstandard pressure rated fittings common in the refrigeration industry.The blast nozzle may be made from cast or machined metal such as brass.The fairing, nozzle housing and discharge nozzle may be cast of avariety of pourable or injectable plastic materials to provide alightweight, rigid and low thermal conduction construction oralternatively a combination of electrically conductive andnon-conductive materials capable of neutralizing or enhancingelectrostatic charges of the fluidized stream.

BRIEF DESCRIPTION OF THE DRAWINGS

The invention will be more readily apparent from the followingdescription of embodiments thereof with reference to the accompanyingdrawings, in which:

FIG. 1 is a flow diagram of a particle blast cleaning and treatingsystem, according to the present invention, wherein a wide variety ofparticulate matter and blast medium may be used.

FIG. 2 is a lateral sectional view of a fluid accelerator andpressurizer apparatus forming part of the system of FIG. 1;

FIG. 3 is an end sectional view of the apparatus of FIG. 2;

FIG. 4 is a fragmentary perspective view of a discharge nozzle connectedin series with the apparatus of FIGS. 2 and 3;

FIG. 5 shows a view in longitudinal cross-section through a dischargegun according to another embodiment of the invention; and

FIG. 6 shows a broken-away exposed view in perspective of parts of thegun of FIG. 5.

DESCRIPTION OF THE BEST MODE

Referring to the drawings and in particular to FIG. 1, there isillustrated a particle blast cleaning and treating system designatedgenerally by reference numeral 1, comprising a tank 2 for making and/orstoring particulate matter 3, a particle sizer 4, a particle meterer 5,a particle fluidizer 6, a fluidizing and high pressure blast mediumsource 7 for providing a pressurized blast medium and supplying theblast medium through a conduit 9 for fluidizing the blast particulatematter, a conduit 8 for transporting the fluidized particulate stream totwo fluid accelerator and pressurizer apparatuses 19 attached in seriesto a discharge nozzle 50, control valves 10, and a deadman switch 11 forturning off and on the particle blast cleaning and treating system 1.

The particulate matter 3 is made, normally continuously or upon demandin the case of water ice or dry ice, or stored, normally in the case ofsand, grit or shot particles, in the particulate tank 2. Thisparticulate matter 3 may either be delivered to the particle fluidizer 6directly or may be sized by the particulate sizer 4 for even metering bythe particle meterer 5 and then fluidized for transport. It will beunderstood by those skilled in the art that, instead of using theparticle meterer 5, the metering of the particles may be accomplished bycontrolling the production rate of the particulate matter 3 in the tank2 and that by fluidization may be incorporated into a common systemconsisting of the tank 2 and the particle sizer 4. Fluidization occursby introduction of a fluidizing medium, which may be gas, liquified gasor liquid, at a controlled pressure from the conduit 9. It will also beunderstood that the lesser but necessarily higher quality medium sourceto be provided in conduit 8 for fluidization and transport mayadvantageously be different from that supplied to conduit 9, whichprimarily provides high pressure energy blast medium to the apparatuses19, in terms of quality, pressure, coldness and dryness. If thefluidized particulate stream must be transported over a long distance toa target surface 18, then it is preferable that at least one fluidaccelerator and pressurizer apparatus 19 be placed at one or moreintermediate positions along conduit 8 to provide boost, as shown inFIG. 1. Otherwise, conveyance to the final delivery outlet isfacilitated by the combined action of the particle fluidizer 6 and onefluid accelerator and pressurizer apparatus 19. In any case, at thefinal delivery outlet of the particle blast cleaning and treating system1, one of the fluid accelerator and pressurizers 19 is attached inseries to a discharge nozzle 50 to allow for the delivery of an evenlydistributed large blast pattern against the target surface 18.

FIGS. 2 and 3 show in greater detail one of the fluid accelerator andpressurizers 19. The conduit 8, preferably a flexible hose, is coupledat an inlet end 21 to a main conduit forming a flow passage 22 extendingthrough a fluid accelerator and pressurizer nozzle housing 20, whichcontains an inner blast nozzle 40. A fairing 23 secures the inner blastnozzle 40 to the main conduit's inner surface or wall 24. The externalsurface 41 of the fairing 23 of the blast nozzle 40 is of an efficientstreamlined, fusiform shape. This fusiform shape has the shape of atorpedo with a "tapered tail" end facing inlet 21 and a "head" endfacing outlet end 28 of the main conduit 22.

The cross-sectional area of the inner surface 24 preferably convergesslightly or remains unchanged from the inlet 21 to an initialconvergent-divergent region or first constriction 25 in the form of aconverging/diverging nozzle located upstream from the inner blast nozzle40. The flow passage 22 then gradually diverges from the throat of thenozzle 25 to provide a first acceleration region 26. Further, the flowpassage 22 is contoured to provide an intermediate region which may beof constant semi-annular cross-sectional area between the inner surface24 and the fairing 23 until a point 27 prior to an outlet end portion 44of the inner blast nozzle 40. It will be understood that the annularcross-sectional area between the flow passage wall 24 and the fairing 23may form a nozzle shape whereby flow straightening, pressure andvelocity conditions may be adjusted. After this point 27, the innerblast nozzle 40 projects from the fairing 23 towards the outlet 28 ofthe flow passage 22. Because the diameter of the flow passage 22 isunchanged during this projection, the cross-sectional area of the flowpassage 22 between the inner surface 24 and the blast nozzle surface 41is greater downstream from the point 27 than it is upstream from thepoint 27. This enlargement provides for a second divergence, and in thecase of a gaseous or liquified gaseous fluidizing blast medium, i.e. acompressible blast medium capable of expansion, an acceleration region29 in the flow passage 22. This arrangement creates a three-dimensionalvarying flow path to avoid plugging and provide acceleration, mixing andeven distribution for a co-axial flow and system pressure. Specifically,the minimum distance between inner surface 24 of the flow passage andthe outer surface of the inner blast nozzle and fairing is based on thespecific particle size and the characteristics of the fluidized streambeing treated, where the minimum preferred distance is 1.5 to 2.0 timesthe mean particle size diameter.

A high pressure blast medium tube 42 penetrates the flow passage 22 andcommunicates with a conduit 43 of the inner blast nozzle 40. The conduit43 is co-axial with the flow passage 22. The blast medium, indicated byreference numeral 48 and in gaseous or liquified gaseous form, capableof partial or whole expansion upon discharge from the inner blastnozzle, is directed through the tube 42 from fluidizing medium source 7.The inner blast nozzle conduit 43 is constant in diameter from the endof blast medium tube 42 to a constriction 45 in the form of a Lavalnozzle throat, which is upstream from the outlet of the inner blastnozzle 40, and which is followed by a divergence region 46.

At some distance downstream from the inner blast nozzle outlet 44, thesurface 24 of passage 22 converges to a constriction 30 and thendiverges, forming an acceleration region 28 of the passage 22. The blastmedium 48 is forced through the nozzle throat 45 at a speed such that itleaves the outlet 44 at supersonic speeds, thus creating an impenetrableflow shear front 47. Between this flow shear front 47 and the walls ofthe nozzle throat 30, an effective or virtual Laval annular nozzle 31 isformed, which serves to accelerate the fluidized particulate stream andwhich may also reduce the size of friable particles to improveacceleration and blast impact.

The cross-sectional area of the flow passage 22, downstream of the point27 is greater than the annular cross-sectional passage area or nozzledefined by the wall of the constriction 30 and the flow front 47.

More particularly, as the gas travels through the nozzle throat 45, thevelocity of the gas may increase. If the velocity of the gas at thethroat of the nozzle throat 45 is subsonic (even though the velocityincreased), then the gas will decelerate. If the velocity of the gas atthe nozzle throat 45 is sonic or above, then the gas will accelerate,which means that the velocity of the gas flow will then be supersonic.When the velocity of the gas leaving the nozzle 40 is supersonic, thegas will form shock waves within the flow shear front 47. For thefluidized stream, this front is practically impenetrable by thefluidized stream, thus forming a virtual wall profile.

This virtual wall profile, in conjunction with the constriction 30,forms a virtual or effective Laval nozzle therebetween, whichaccelerates the fluidized stream by exerting an inductive effect on thefluidized stream, thus producing a useful pressure boost for subsonictransport and/or increased velocities for a combined gas/particulatesupersonic flow.

The shear forces of the high energy blast air at the flow front transferkinetic energy from the high velocity blast air to the transport gas andthe ice particles of the fluidized stream, thereby increasing theirrespective velocities rather than by random turbulent mixing and contactof particles with solid wall surfaces, which would cause attrition anderosion and would not be conductive to effective subsequent nozzleperformance.

The inductive effect of the pressure boost by the virtual nozzle asdescribed above is directly related to the volume of transport aircarrying the particles through the annular throat of the virtual nozzle.When the flow is nil or small, the virtual nozzle is unchoked and thepressure boost provided by the first inner nozzle kinetic energy will benear one atmosphere, (14.7 psi). When the transport/particle volume flowis increased, the pressure boost is less as the virtual nozzle presentsa pressure resistance to increasing flow. Thus, there is limitedpressure boost available from an inductive nozzle which varies betweenmax. 14 psi and 0 depending upon the flow of transport air withparticles.

Under non-pressurized system conditions where the starting pressure atthe source of ice particle production with adequate transport air volumeis at atmospheric pressure (14.7 PSIA), the inductive effect willproduce a vacuum of approximately 12.0 PSIA (0 PSIA is a full vacuum)located just prior to the outlet of the high energy blast nozzle.

Between this point and the point just after the throat of the virtualnozzle, the high energy blast air, transport gas and particulate matterwill mix, and the part of the energy of the high energy blast air istransferred to the transport gas, thereby raising the pressure of thetransport gas. Under normal operating conditions and with suitablenozzle configuration, the pressure of the mix including high energyblast air, transport gas and particulate matter can rise to as high as16 PSIA.

Subsequently, the pressure of the mix has to decrease to atmosphericpressure, where the mix is finally discharged into the environment.

The foregoing operating conditions are suitable for ice blasting, but,such conditions can be modified if required.

As discussed above, when the flow velocity through the Laval nozzlethroat formed by the constriction 45 is sonic, the resulting flow willbe supersonic, which results in a better work effect. In the case of thevirtual nozzle, the inventor has determined that a pressure of 16 PSIAis not high enough to generate a supersonic flow. Instead, what isrequired is a pressure differential above atmospheric, between 40-50PSI, which means the pressure at the point just after the throat of thevirtual nozzle should have a pressure of 54.7-64.7 PSIA.

The inventor has also determined that greater pressure differentialabove 40-50 PSI can result in higher supersonic speeds and thereforebetter work effect.

In the case of ice, and in order to avoid melting, agglomeration andplugging particles must not be exposed to warm moist air. However, cooldry air (also known as "high quality air"), is expensive to produce. Thepresent apparatus requires the use of high quality air only as thetransport gas, which normally only accounts for 20% or less of the totalvolume of gas in the system. The balance of the 80% or more is highenergy blast air from the blast nozzle 40, which does not have to behigh quality air.

The particulate matter does not have to travel at high speeds throughoutthe apparatus. It is only necessary that the particulate matter travelsat a high speed at the discharge point. This facilitates avoidance ofunwanted side effects such as conduit erosion, turbulence, mixing,increased friction, loss of efficiency, particle destruction, productionof snow and lessened work effect. Also, large transportable particlesmay be more efficiently transported and any reduction in size useful foracceleration and work effect may be done by adjusting shear forceintensity in the jet fluid apparatus. The particulate matter isdelicately transported along at a speed sufficient to avoid plugging butinsufficient to create the desired blast effect, thereby allowing formaximal preservation of particles.

FIG. 4 depicts a perspective view of the discharge nozzle 50 connectedin series to one of the fluid accelerator and pressurizers 19. With thedischarge nozzle 50 attached in series to the fluid accelerator andpressurizer 19 and sufficient pressure of all flows at or after theeffective nozzle there is a further expansion and fluidic energytransfer and acceleration. This effective energy transfer from the blastmedium 48 to the particles in the fluidized stream in the form ofvelocity assists in producing a linear strip or fan pattern having ahigh and even concentration of particles for impact. In such anarrangement, the duct profile after initial mixing in the main conduitmakes a transition from a diverging annular flow to a transverselyelongate, diverging rectangular form 51. The discharge nozzle 50 mayhave alternative forms, e.g. a circular, oblong or square form. In thisway, the flow may be accelerated to sonic or supersonic speeds with anoptimum pattern. For such an expansion to occur, it is necessary thatthe stream speed through the effective nozzle throat is sonic, and theupstream pressures are balanced as is described below in the example forwater ice. Further, the transitional nozzle profile must considermaintaining even multi-phase distribution, mixing for particleacceleration, and dimensional criteria for plugging and pressurecontrol.

A more complete understanding of the present invention can be obtainedby referring to the following example of water ice or dry ice blastingof surfaces, which example is not intended to be limitative of theinvention. In a conventional environment of ice blasting apparatus andmethodology, comprising mechanisms for ice making, ice particle sizing,metering and fluidizing or ice making, ice particle sizing andfluidizing using high quality pressurized air (20% cold and dry air, 80%ambient air), fluid accelerator and pressurizers 19 are used totransport a fluidized ice particle stream over long distances to a finaldelivery and discharge point, and also to discharge the fluidized streamagainst a target surface.

In the ice blasting context, from the nozzle throat 25 there is slightacceleration of the incoming fluidized stream of ice particles and air,which is fed in the range from a moderate vacuum to 15-25 psig. Theresulting fluid stream is then directed along the body of the innerblast nozzle 40 and the fairing 23 as a partial annular flow.

At the next acceleration region 29, the fluidized stream becomes a fullannular flow and is again slightly accelerated. The partial and fullannular flows are designed to minimize plugging and maximize energytransfer from the blast medium stream. The fairing 23 prevents theformation of velocity differentials that cause deposition and plugging.

The blast medium 48, which in this case consists of low quality cool dryair, is introduced through the blast medium tube 42 and the inner blastnozzle conduit 43 at 100-450 psig. At the inner blast nozzle throat 45,the air is forced to reach sonic speed. Following this point, the blastmedium decompresses reaching a supersonic speed and forms the effectivenozzle. The annular fluidized stream, travelling at subsonic speed, isunable to penetrate the flow front 47 and, due to the shear andinductive forces of the flow front 47 moving at a high speed and theconvergence of the surface 24 of the passage 22 at the nozzle throat 30,the annular fluidized stream is significantly accelerated and itspressure is boosted up to 15 psig or greater. The configuration of thiseffective nozzle is dependent upon the proximity of the inner blastnozzle outlet 44 to the convergence of the passage 22 at nozzle throat31, the velocities and flows of the blast medium 48 and the fluidizedstream. The ratio between the pressures and volumes of the incomingfluidized stream and the blast medium are set at a range of 1:7 to 1:35for the pressures and 1:7 to 1:14 for the volumes. It is preferable butnot necessary that the ratio of these pressures remain in this range. Alow ratio of volumes will result in choking at the nozzle throat 30, arise in upstream pressure and consequently an interference with upstreamfluidization and transport. If the ratio is too high, there will beinefficient use of the high energy blast medium and excessive volumes ofthe total mixed fluidized flow may also result in choking in throat 30or subsequent nozzles.

FIGS. 5 and 6 shows a modification of the apparatus of FIGS. 2 to 4.

In the apparatus of FIGS. 5 and 6, there is provided a gun indicatedgenerally by reference numeral 60, which comprises a nozzle housing orbody 62 provided with a handle 64. A flow passage 66 for the flow of afluidized stream of transport gas and particulate material, for example,ice particles, is formed preferably with a first convergent-divergentconstriction or Laval nozzle 68, with a blast nozzle 70 projecting intothe flow passage 66. The blast nozzle 70 is provided with a fairing 72,and the flow passage 66, beyond the Laval nozzle 68, has a section ofconstant or varying cross-sectional area 74 extending in the downstreamdirection from the nozzle 68 to an enlargement 76, at which the nozzle70 projects from the fairing 72 to provide the fluid passage 76 with anannular shape.

The blast nozzle 70 has an end portion 77 which includes aconvergent-divergent constriction in the form of a Laval nozzle 78 foraccelerating to supersonic speed a blast medium supplied to the nozzle70 through a supply tube 80.

The blast nozzle 70 discharges into a converging passage portion 82,which communicates with the fluid passage 66 and extends to aconstriction 83 communicating with a passage 84 of substantiallyconstant cross-section. The converging passage portion 82 and thepassage portion 84 extend through a component forming a nozzle memberindicated generally by reference numeral 86, which has a cylindricalportion 88 extending into the body 62 and an annular flange portion 90extending around one end of the cylindrical portion 88.

More particularly the nozzle member 86 is rotatably mounted in anelectrically conductive connector insert 92, which has an externallyribbed cylindrical portion 94 embedded in the body 62 and a radiallyoutwardly extending annular flange 96, which abuts the flange 90 of thenozzle member 86.

The connector insert 92 makes electrical contact with a conductivelining 98 on the wall of the fluid passage 66, and the conductive lining98, in turn, makes electrical contact with a pair of threaded connectorsindicated generally by reference numeral 100, which are formed in onepiece of metal and embedded in the body 62. The insert member 86 is inthreaded engagement with a threaded end portion 102 of a dischargenozzle indicated generally by reference numeral 104. The end portion 102is provided on a tube 106, which is formed with an annular flange 108abutting the nozzle member 86, and which extends through a plastic body110 of the nozzle 104. The tube 106 forms a flow passage which initiallyhas a circular cross-section, which merges into a rectangularcross-section at a discharge end 112.

Alternatively, for more convenient construction of the nozzle 104, thetube 106 may be replaced by a transitional cross-section lining, whichmay be made of stamped metal or any suitable conductive material incontact with bushing 114 and connected to the bushing 114 via threads.The conductive lining may be made by metallizing a plastic and the sameapplies to passage way 66. Also, the outside of the gun 60 and thenozzle 104 may be metallized.

The tube 106 is made of metal or made conductive as described above, andmakes electrical contact with a conductive metal bushing 114. If thelining of nozzle 104 is not conductive, the busing may be connected by agrounding conductor 116 to a conductive strip 118 at the discharge end112 of the discharge nozzle 104. Similarly if liner 98 of the flowpassage 66 is not conductive, a grounding conductor 117 may connect thethreaded connectors 100 to the ribbed cylindrical portion 94 of theconductive connector insert. The electrically conductive strip 118 isgrounded through the conductor 117 and the conductive bushing 114. Thestrip 118 is useful, if the tube 106 terminates before the mouth of thenozzle 104.

The strip 118 is preferably formed to contact both the interior flowpath of nozzle 104, and its outer surface in order to cancel staticcharge build-up.

In certain cases charge build-up is beneficial to work effect; wherethere is no hazard, for example from explosion, components such as thenozzle 104 may be changed, or grounding conductors may be interrupted byswitching (not shown).

The connector insert 92 is connected through a conductor 120 to a switch122, which is in turn connected through a conductor 124 to a connectorplug 126 for connection to ground. The connecting member 100 is groundedby a conductor 128 through the plug 126.

The plug 126 is connected back to the ground connection of a plantsupplying blast and transport medium, particles and its control system.The plug 126 may also be connected to a local ground and, as required,to the work piece. In this manner all of the chosen components asdescribed above are safely grounded.

The switch 122 may have several functions. As described above, it may beused to temporarily interrupt grounding on certain components but alwayshaving fail safe to full grounding.

FIG. 5 shows switch 122 having two "deadman" type switches 132 and 134.The following is an example of such switch use for operationalconvenience and efficiency.

When the particle making and gas transport system has been activated butno switches used, there will be only a minimum amount of transport airbeing fed from conduit 8 (FIG. 1), into flow passage 66 (FIG. 5) and aminimum amount of high pressure blast medium from conduit 48 whichenters supply tube 80 of FIG. 5.

This establishes a ready "idle" state, and provides inductive flow forthe transport conduit to ensure against plugging and in the case ofwater ice, also melting.

Either of the switches 132 or 134 may be programmed to provide highvelocity air only to clear the work piece prior to particulate blastingor after a section of the work is performed, or particulate blasting atpre-set rates and pressures from the system described in FIG. 1.

The cylindrical portion 88 of the nozzle member 86 is sealed to theelectrical connector 92 by means of a sealing ring 135, which isrecessed in the cylindrical surface of the cylindrical portion 88, andthe cylindrical portion 88 tapers at its inner end so that the wall ofthe converging passage portion 82 merges smoothly with the inner surfaceof the lining 98 so as to counteract turbulence in the flow of materialthrough the flow passage 66.

The flange 96 of the electrical connector 92 is formed with a pair ofopposed arcuate slots 136, to allow articulation of the tube 106 and thenozzle 104 for work convenience and a pair of frangible bolts 138 extendthrough holes 140 in the flange 90 of the insert 86 and through theslots 136 into threaded engagement with retaining nuts 142. The bolts138 are each formed with a weakened portion 144, which will break whenthe bolts 138 are subjected to a predetermined tensile load for pressuresafety as described below.

The blast nozzle 70, the fairing 72 and the fluid passage 66 operate ina manner which corresponds to that described above with reference toFIGS. 2 to 4 and which therefore is not described in detail herein.Fluid discharged through an end portion 78 serves to form a flow shearfront 146, similar to the flow shear front 47 of FIG. 2, and the flowshear front 146, in conjunction with converging passage portion 82 andconstriction 83, form, likewise, a virtual or effective nozzle foraccelerating the fluidized stream.

If the flow passage portion 84 should inadvertently become choked andplugged by deposition of particulate material, then the supply of blastmedium at high pressure through the tube 80 could result in the creationof an abnormally high and dangerous pressure within the flow passage 66and the components upstream of the flow passage 66 communicatingtherewith. To prevent this occurrence, the bolts 138 are formed withweakened portions 144, so that the bolts 138 will fail and the insertmember 86 will be blown away from the body 62 if an unacceptably highexcess pressure occurs in the flow passage 66.

The flange 90 of the insert 86 is penetrated by a pair of electricallyconductive brushes 150, which make electrical contact, at opposite endsthereof, with the flange 96 of the electrical connector 92 and with theflange 108 on the tube 106. In this way, the tube 106 and, through thegrounding conductor 116, the end conductor 118, are grounded through theelectrical connector 92.

The bolts 138 are slidable to and fro along the slots 136 in order toallow the insert member 86, and therewith the discharge nozzle 104, tobe rotated relative to the body 62 for correspondingly varying theorientation of the discharge from the discharge nozzle 104.

It will be understood from the foregoing description and apparent thatvarious modifications and alterations may be made in the form,constriction and arrangement of the parts thereof without departing fromthe spirit and scope of the invention or sacrificing all of its materialadvantages, the form herein described being merely preferred embodimentsthereof.

I claim:
 1. A fluid jet accelerator/pressurizer apparatus foraccelerating and pressurizing a fluidized stream of particulate matter,comprisinga nozzle housing defining a main conduit; said main conduitforming a passage for the flow of the fluidized stream through saidnozzle housing; said main conduit having a constriction formed by aconvergent-divergent region of said main conduit for effectingacceleration of the fluidized stream; an inner blast nozzle provided insaid main conduit upstream of and directed in a downstream directiontowards said constriction; and a means for discharging a blast mediumfrom said inner blast nozzle at a speed sufficient to form within thefluidized stream a flow front which is impenetrable by the fluidizedstream and which co-operates with said constriction to accelerate thefluidized stream.
 2. The apparatus of claim 1, wherein said nozzle has astreamlined fairing.
 3. The apparatus of claim 2, wherein said mainconduit further comprises a further flow constriction in said passageupstream from said inner blast nozzle for accelerating the fluidizedstream.
 4. The apparatus of claim 2, wherein said main conduit includesa wall defining said passage; said inner blast nozzle has an outlet endportion spaced from said wall; and said nozzle housing, said fairing andsaid wall define a length of said passage along which said passage has aconstant cross-sectional area.
 5. The apparatus of claim 4, wherein saidwall and said flow front define therebetween a cross-sectional area lessthan a cross-sectional area defined between said wall and said outletend of said inner blast nozzle.
 6. The apparatus of claim 1, whereinsaid inner blast nozzle comprisesan external body profile of a fusiformshape for efficient guidance of the flow path of the fluidized stream;and an internal inner blast nozzle conduit for delivery of the blastmedia axially of said main conduit, said internal inner blast nozzleconduit having an outlet and an internal convergent region located atsaid outlet for accelerating the blast media.
 7. The apparatus of claim1, further comprising a discharge nozzle for controlling and enhancingthe acceleration and exit of said fluidized stream from said mainconduit towards a target surface, said discharge nozzle having areceiving end defining an opening communicating with said main conduit,a discharging end defining a transversely elongate opening, and aconduit portion connecting said receiving and discharging ends.
 8. Theapparatus of claim 1, wherein said flow passage has a grounded lining tocounteract build-up of electrostatic charge on said nozzle housing. 9.The apparatus of claim 8, having conductive parts within said flowpassage and conductors interconnect said conductive parts for groundingsaid conductive parts.
 10. The apparatus as claimed in claim 8, whereinsaid constriction is provided on a component separate from said nozzlehousing; and said apparatus includes retaining members which realizablysecure said component to said nozzle housing and which retaining membersare frangible to release said component from said nozzle housing inresponse to an excess pressure in said flow passage.
 11. The apparatusof claim 8, further comprisinga discharge nozzle communicatingdownstream of said constriction with said flow passage; and a rotatableconnection between said nozzle housing and said discharge nozzlepermitting rotation of said discharge nozzle.
 12. The apparatus of claim11, further comprisingan electrically conductive flow passage in saiddischarge nozzle; and a grounded conductor in said nozzle housing andelectrical brushes interconnecting said electrically conductive flowpassage and said grounded conductor.
 13. A fluid jetaccelerator/pressurizer apparatus for accelerating and pressurizing afluidized stream of particulate matter, comprisinga nozzle housingdefining a main conduit; said main conduit forming a passage for theflow of the fluidized stream through said nozzle housing; said mainconduit having a constriction means for effecting acceleration of thefluidized stream; an inner blast nozzle provided in said main conduitand directed in a downstream direction towards said constriction means;and a means for discharging a blast medium from said inner blast nozzleat a speed sufficient to form within the fluidized stream a flow frontwhich is impenetrable by the fluidized stream and which co-operates withsaid constriction means to accelerate the fluidized stream.
 14. A fluidjet accelerator/pressurizer apparatus for accelerating and pressurizinga fluidized stream or particulate matter, comprisinga nozzle housingdefining a main conduit; said main conduit forming a passage for theflow of the fluidized stream through said nozzle housing; said mainconduit having, in succession in the direction of flow of the fluidizedstream, an inlet end, a first constriction formed by aconvergent-divergent region of said main conduit for effecting aninitial acceleration of the fluidized stream, an intermediate region, asecond constriction for effecting a further acceleration of thefluidized stream and an outlet end; an inner blast nozzle in said mainconduit for discharging a blast media at high speeds through said secondconstriction towards said outlet end of said main conduit; and a meansfor discharging a blast medium at supersonic speed from said inner blastnozzle so as to form within the fluidized stream a flow front which isimpenetrable by the fluidized stream and which co-operates with saidconstriction to accelerate the fluidized stream.
 15. The apparatus ofclaim 14, wherein said nozzle has a streamlined fairing.
 16. Theapparatus of claim 14, wherein said main conduit has a wall definingsaid passage; said inner blast nozzle has an outlet end portion spacedfrom the wall of said main conduit; and said intermediate region has across-sectional passage area, defined by said nozzle housing, said innerblast nozzle and said fairing, which cross-sectional passage area isconstant along the length of said intermediate region.
 17. The apparatusof claim 16, wherein said main conduit further comprises a furtherpassage region beyond said intermediate region and extending along saidoutlet end portion of said inner blast nozzle; and said further passageregion has a greater cross-sectional passage area than the annularcross-sectional passage area between the wall and the flow front. 18.The apparatus of claim 14, wherein said inner blast nozzle comprisesanexternal body profile of a fusiform shape for efficient guidance of theflow path of the fluidized stream; and an internal inner blast nozzleconduit for the delivery of the blast media axially of said mainconduit; said internal inner blast nozzle conduit having an outlet andan internal convergent region located at said outlet for acceleratingthe blast media.
 19. The apparatus of claim 14, further comprising adischarge nozzle for controlling and enhancing the acceleration and exitof said fluidized stream from said main conduit towards a targetsurface; said discharge nozzle having a receiving end defining anopening communicating with said main conduit, a discharging end defininga transversely elongate opening, and a conduit portion connecting saidreceiving and discharging ends.